A termék adatai:
| ISBN13: | 9781108420600 |
| ISBN10: | 1108420605 |
| Kötéstípus: | Keménykötés |
| Terjedelem: | 566 oldal |
| Méret: | 249x175x34 mm |
| Súly: | 1070 g |
| Nyelv: | angol |
| 720 |
Témakör:
Dynamics of Flexible Aircraft
Coupled Flight Mechanics, Aeroelasticity, and Control
Sorozatcím:
Cambridge Aerospace Series;
52;
Kiadó: Cambridge University Press
Megjelenés dátuma: 2023. július 13.
Normál ár:
Kiadói listaár:
GBP 99.99
GBP 99.99
Az Ön ára:
43 465 (41 396 Ft + 5% áfa )
Kedvezmény(ek): 10% (kb. 4 830 Ft)
A kedvezmény csak az 'Értesítés a kedvenc témákról' hírlevelünk címzettjeinek rendeléseire érvényes.
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Beszerezhetőség:
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Rövid leírás:
Explore the interface between aeroelasticity, flight dynamics and control in this fresh approach, featuring numerous hands-on examples.
Hosszú leírás:
Explore the connections among aeroelasticity, flight dynamics, and control with an up-to-date multidisciplinary approach. New insights into the interaction between these fields, which is a distinctive feature of many modern aircraft designed for very high aerodynamic efficiency, are fully illustrated in this one-of-a-kind book. Presenting basic concepts in a systematic and rigorous, yet accessible way, this book builds up to state-of-the-art models through an intuitive step-by-step approach. Both linear and nonlinear attributes are covered and, by revisiting classical solutions using modern analysis methods, this book provides a unique perspective to bridge the gap between disciplines. Numerous original numerical examples, including online source codes, help to build intuition through hands-on activities. This book will empower the reader to design better and more environmentally friendly aircraft, and is an ideal resource for graduate students, researchers, and aerospace engineers.
Tartalomjegyzék:
1. Introduction; 2. The non-stationary atmosphere; 3. Dynamics of elastically-supported rigid airfoils; 4. Dynamics of rigid aircraft in a non-stationary atmosphere; 5. Dynamics of flexible aircraft with quasi-steady deformations; 6. Dynamics of flexible aircraft with small-amplitude vibrations; 7. Time-domain unsteady aerodynamics for low-speed flight 8. Geometrically-nonlinear composite beams; 9. Dynamics of very flexible aircraft; 10. Feedback control; 11. Experimental testing; Appendices.
